ATTITUDE CONTROL DATA CREATING METHOD, AND ATTITUDE CONTROL SYSTEM APPLYING THE METHOD
    1.
    发明申请
    ATTITUDE CONTROL DATA CREATING METHOD, AND ATTITUDE CONTROL SYSTEM APPLYING THE METHOD 有权
    态度控制数据创建方法以及应用方法的态度控制系统

    公开(公告)号:US20090218449A1

    公开(公告)日:2009-09-03

    申请号:US12300449

    申请日:2007-05-02

    IPC分类号: B64G1/28 B64G1/24

    摘要: In order to control an attitude of a movable object having a flexible member (50) through an attitude maneuver, first, based on vibration of the flexible member at the time of the attitude maneuver, for example, a sampling function including no frequency components equal to or higher than a particular frequency is obtained. With the use of the sampling function, a control target value is created as a previously-frequency-shaping-type feedforward control law. Based on the control target value, attitude control data is created. The attitude control data can be used for the attitude maneuver with respect to the movable object.

    摘要翻译: 为了通过姿态机动来控制具有柔性构件(50)的可移动物体的姿态,首先,基于姿态机动时的柔性构件的振动,例如,不包括频率成分相等的取样函数 达到或高于特定频率。 利用采样功能,创建控制目标值作为先前频率整形型的前馈控制定律。 基于控制目标值,创建姿态控制数据。 姿态控制数据可以用于相对于可移动物体的姿态操纵。

    Attitude control data creating method, and attitude control system applying the method
    2.
    发明授权
    Attitude control data creating method, and attitude control system applying the method 有权
    态度控制数据创建方法,姿态控制系统应用该方法

    公开(公告)号:US08186627B2

    公开(公告)日:2012-05-29

    申请号:US12300449

    申请日:2007-05-02

    IPC分类号: B64G1/36

    摘要: In order to control an attitude of a movable object having a flexible member (50) through an attitude maneuver, first, based on vibration of the flexible member at the time of the attitude maneuver, for example, a sampling function including no frequency components equal to or higher than a particular frequency is obtained. With the use of the sampling function, a control target value is created as a previously-frequency-shaping-type feedforward control law. Based on the control target value, attitude control data is created. The attitude control data can be used for the attitude maneuver with respect to the movable object.

    摘要翻译: 为了通过姿态机动来控制具有柔性构件(50)的可移动物体的姿态,首先,基于姿态机动时的柔性构件的振动,例如,不包括频率成分相等的取样函数 达到或高于特定频率。 利用采样功能,创建控制目标值作为先前频率整形型的前馈控制定律。 基于控制目标值,创建姿态控制数据。 姿态控制数据可以用于相对于可移动物体的姿态操纵。

    Attitude change control method, attitude change control system, attitude change control program and program recording medium
    3.
    发明授权
    Attitude change control method, attitude change control system, attitude change control program and program recording medium 有权
    姿态改变控制方法,姿态变化控制系统,姿态变化控制程序和程序记录介质

    公开(公告)号:US08038101B2

    公开(公告)日:2011-10-18

    申请号:US12027769

    申请日:2008-02-07

    IPC分类号: B64G1/28

    CPC分类号: B64G1/286 G05D1/0883

    摘要: Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.

    摘要翻译: 公开了一种姿态改变控制系统,其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩,通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓 来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态,从而控制CMG 40改变姿态 太空工艺动力50目标方向。

    Attitude Change Control Method, Attitude Change Control System, Attitude Change Control Program and Program Recording Medium
    4.
    发明申请
    Attitude Change Control Method, Attitude Change Control System, Attitude Change Control Program and Program Recording Medium 审中-公开
    态度变化控制方法,态度变化控制系统,态度变化控制程序和程序记录介质

    公开(公告)号:US20090039202A1

    公开(公告)日:2009-02-12

    申请号:US12191389

    申请日:2008-08-14

    IPC分类号: B64G1/28 B64G1/24

    CPC分类号: B64G1/286 B64G2001/245

    摘要: Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.

    摘要翻译: 公开了一种姿态改变控制系统,其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩,通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓 来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态,从而控制CMG 40改变姿态 太空工艺动力50目标方向。

    ATTITUDE CHANGE CONTROL METHOD, ATTITUDE CHANGE CONTROL SYSTEM, ATTITUDE CHANGE CONTROL PROGRAM AND PROGRAM RECORDING MEDIUM
    5.
    发明申请
    ATTITUDE CHANGE CONTROL METHOD, ATTITUDE CHANGE CONTROL SYSTEM, ATTITUDE CHANGE CONTROL PROGRAM AND PROGRAM RECORDING MEDIUM 有权
    态度变化控制方法,态度变化控制系统,态度变化控制程序和程序记录介质

    公开(公告)号:US20080203230A1

    公开(公告)日:2008-08-28

    申请号:US12027769

    申请日:2008-02-07

    IPC分类号: B64G1/28

    CPC分类号: B64G1/286 G05D1/0883

    摘要: Disclosed is an attitude change control system that is designed to efficiently output a torque for attitude change of a space craft using CMGs and realizes a real time CMG driving rule. A CMG gimbal steering law 15 generates target profiles for setting angle and angular velocity for each gimbal by applying an anisotropic weighted gradient method based upon the necessary torque calculated by a feed back controller 13 and a feed forward controller 14 from the angle and angular velocity in the target direction from the attitude navigator 12 and the current angle and angular velocity of the space craft estimated by the attitude estimator 11 as well as the current condition of each gimbal from the CMG 40, thereby controlling the CMG 40 for changing the attitude of the space craft dynamics 50 to the target direction.

    摘要翻译: 公开了一种姿态改变控制系统,其被设计为有效地输出用于使用CMG的航天飞机姿态变化的扭矩并实现实时CMG驱动规则。 CMG万向节转向规则15通过基于由反馈控制器13和前馈控制器14计算出的必要扭矩,通过从角度和角速度来计算每个万向节的角度和角速度来生成用于设置每个万向节的角度和角速度的目标轮廓 来自姿态导航仪12的目标方向以及由姿态估计器11估计的航天飞船的当前角度和角速度以及来自CMG 40的每个万向节的当前状态,从而控制CMG 40改变姿态 太空工艺动力50目标方向。

    Power conversion device
    6.
    发明授权
    Power conversion device 有权
    电源转换装置

    公开(公告)号:US08674636B2

    公开(公告)日:2014-03-18

    申请号:US13126410

    申请日:2009-10-26

    IPC分类号: H02P6/00 H02P6/14

    摘要: A power conversion device for a vehicle includes: a power module that includes a switching device and, upon operation of the switching device, converts DC power into AC power to be supplied to an electric machine for driving a vehicle; a capacitor module that includes a smoothing capacitor element, an input-side power source terminal for receiving DC power, and an output-side power source terminal for supplying DC power to the power module; and a noise removal capacitor for removing noise, wherein: the noise removal capacitor is built in the capacitor module, and the noise removal capacitor is electrically connected to the input-side power source terminal in a position where a distance between a connection position of the noise removal capacitor and the input-side power source terminal is less than a distance between a connection position of the noise removal capacitor and the output-side power source terminal of the capacitor module.

    摘要翻译: 一种用于车辆的电力转换装置,包括:功率模块,其包括开关装置,并且在所述开关装置的动作时,将直流电力转换为交流电力,供给到用于驱动车辆的电动机器; 包括平滑电容器元件的电容器模块,用于接收直流电力的输入侧电源端子和用于向功率模块提供直流电力的输出侧电源端子; 以及用于消除噪声的噪声消除电容器,其中:噪声消除电容器内置在电容器模块中,并且噪声消除电容器在输入侧电源端子的连接位置之间的距离处电连接到输入侧电源端子 噪声消除电容器和输入侧电源端子小于噪声去除电容器的连接位置和电容器模块的输出侧电源端子之间的距离。

    Titanium-containing solution, catalyst for polyester preparation, process for preparation of polyester resin, and blow molded product comprising polyester
    7.
    发明申请
    Titanium-containing solution, catalyst for polyester preparation, process for preparation of polyester resin, and blow molded product comprising polyester 审中-公开
    含钛溶液,聚酯制备用催化剂,聚酯树脂的制造方法以及包含聚酯的吹塑成型体

    公开(公告)号:US20070100124A1

    公开(公告)日:2007-05-03

    申请号:US10560923

    申请日:2004-06-16

    IPC分类号: C08G63/00

    摘要: The present invention provides a titanium-containing solution having excellent storage stability and containing the titanium component at a high concentration; a catalyst for polyester preparation exhibiting excellent supply uniformity and high catalyst performance, which does not have adverse effect on the quality of the aliphatic diols to be recovered and recycled; and a catalyst for polyester preparation having high catalyst activity and high molding stability. The invention also provides a process for preparation of a polyester resin using the catalyst, and a blow molded product comprising the polyester resin. A first embodiment of the invention is a titanium-containing solution which contains titanium, an aliphatic diol and a polyhydric alcohol having a valency of 3 or greater. A second embodiment of the invention is a titanium-containing solution which has the titanium particle size in the solution within a specific range.

    摘要翻译: 本发明提供了具有优异的储存稳定性并且含有高浓度的钛成分的含钛溶液; 用于聚酯制备的催化剂,其表现出优异的供应均匀性和高催化剂性能,对待回收和再循环的脂族二醇的质量没有不利影响; 和具有高催化剂活性和高成型稳定性的聚酯制备用催化剂。 本发明还提供了使用该催化剂制备聚酯树脂的方法和包含聚酯树脂的吹塑制品。 本发明的第一个实施方案是含有钛,脂肪族二醇和三价以上的多元醇的含钛溶液。 本发明的第二个实施方案是一种含钛溶液,其溶液中的钛颗粒尺寸在特定范围内。

    Polyester resin and catalyst for polyester production, process for producing polyester resin with the catalyst, polyester resin obtained with the catalyst, and hollow molded container comprising the polyester resins
    9.
    发明授权
    Polyester resin and catalyst for polyester production, process for producing polyester resin with the catalyst, polyester resin obtained with the catalyst, and hollow molded container comprising the polyester resins 有权
    用于聚酯生产的聚酯树脂和催化剂,用催化剂生产聚酯树脂的方法,用催化剂获得的聚酯树脂和包含聚酯树脂的中空成型容器

    公开(公告)号:US07300998B2

    公开(公告)日:2007-11-27

    申请号:US10504529

    申请日:2003-02-13

    IPC分类号: C08G63/02

    摘要: The object of the present invention is to provide a high quality polyester resin having high productivity, stability and safety, a catalyst for polyester production with high catalytic activity, a method for producing the polyester resin with the catalyst, a polyester resin obtained with the catalyst, and a hollow molded container having the polyester resin. The polyester resin of the present invention satisfies specific parameters regarding polymerizability, stability, and metal content. The catalyst for polyester production satisfies specific parameters. The catalyst particularly preferably has: (a) a solid titanium-containing compound which has a maximum solubility in ethylene glycol of 1,000 ppm or more in terms of converted titanium amount when dissolved in ethylene glycol with heating at 150° C., and which has titanium, oxygen, carbon, and hydrogen, and optionally an alkali metal, and has a Ti—O—C bond; and (b) an alkali metal compound, the molar ratio of the alkali metal atoms to the titanium atom in the catalyst being in the range of 20/1 to 0.1/1.

    摘要翻译: 本发明的目的是提供一种具有高生产率,稳定性和安全性的高品质聚酯树脂,具有高催化活性的聚酯生产催化剂,用催化剂生产聚酯树脂的方法,用催化剂得到的聚酯树脂 和具有聚酯树脂的中空成型容器。 本发明的聚酯树脂满足关于聚合性,稳定性和金属含量的具体参数。 聚酯生产催化剂满足具体参数。 催化剂特别优选具有:(a)当在150℃下加热溶解在乙二醇中时,以乙二醇的最大溶解度为1000ppm以上的钛的固体含量的化合物, 钛,氧,碳和氢,以及任选的碱金属,并具有Ti-OC键; 和(b)碱金属化合物,催化剂中碱金属原子与钛原子的摩尔比在20/1至0.1 / 1的范围内。